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ELECTRON R/B

NORAD 101147 Rocket Body LEO 2026-239D
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🛰️ Orbital Parameters
Perigee
167 km
Apogee
495 km
Inclination
97.4°
Period
91.2 min
Mean Motion
15.79729557 rev/day
TLE Epoch
2026-10-24 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude331 km
Orbital Velocity27,763 km/h
Velocity7.71 km/s
Orbital Period91 minutes
Orbits / Day15.80
Eccentricity0.0245
Semi-Major Axis6,702 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-10-23
Launch Site
Rocket Lab Launch Complex 1, New Zealand
Int'l Designator
2026-239D
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
ELECTRON R/B is a spent rocket body associated with United States, launched on 2026-10-23 from Rocket Lab Launch Complex 1, New Zealand on the Hawk 16A/B/C launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 167 km and 495 km with an inclination of 97.4°. It travels at approximately 27,763 km/h (7.71 km/s), completing one full orbit every 91 minutes — that’s roughly 15.80 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Spent rocket bodies like ELECTRON R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
ELECTRON R/B orbits at an average altitude of 331 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of ELECTRON R/B’s average altitude, there are currently 1,009 active payloads and 37 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 5.3% of all active satellites. With an inclination of 97.4°, ELECTRON R/B passes over latitudes between 97.4°N and 97.4°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,286 active satellites in total, of which 955 share a similar altitude band with ELECTRON R/B.
🔗 Spent Rocket Body

This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.

❓ Frequently Asked Questions
ELECTRON R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 331 km altitude. Its 97.4° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 91 minutes, travelling at 27,763 km/h.
ELECTRON R/B (NORAD ID 101147) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
ELECTRON R/B was launched on 2026-10-23 from Rocket Lab Launch Complex 1, New Zealand. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks ELECTRON R/B (NORAD ID 101147) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
ELECTRON R/B travels at approximately 27,763 km/h (17,251 mph) — roughly 7.71 km/s. It completes 15.80 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 sunrises and sunsets every 24 hours.